What was found
WHILE IN C CHECK, MAINTENANCE FOUND CRACK IN CUTOUT, NR 4 SLAT COVE PANEL, JUST O/B OF ACTUATOR ROD END. INSTALLED REPAIR PER SRM 51-30-2, 51-40-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE IN C CHECK, MAINTENANCE FOUND CRACK IN CUTOUT, NR 4 SLAT COVE PANEL, JUST O/B OF ACTUATOR ROD END. INSTALLED REPAIR PER SRM 51-30-2, 51-40-2.